DESIGN AND CALCULATION OF THE DEICING SYSTEM FOR SMALL PASSENGER AIRCRAFT TO TAKE-OFF WEIGHT 2000 kg

Abstract

The role and aim of the thesis was to design and calculate the deicing system small transport aircraft to take-off mass of 2000 kg. In the introduction it is dismantled icing problems, its effect on the airplane and flight characteristics, eliminating the possibility of frost in flight and analysis of the current state of de-icing systems described in specific types of aircraft. The core of the work consists of three separate sections. The second chapter consists of the actual design of the mechanical de-icing system leading edges of wings and tail surfaces. The third chapter discusses the design of the electrical system defrost windscreens cockpit, propeller leading edges, the entry of air into the powerplant and defrost flaps in the air duct nacelle. Last of the chapters deals with the design of detection and alarm icing. The work includes calculations of specific components of the whole system and also by pictures and diagrams of the proposed system.